An engine installation system includes two aftward members and two forward members. Each member is connected to a different bootstrap on one end and has a pivotable connection to a pylon on the other end. There is a link that connects one forward member with one aftward member, and another link that connects the other forward member with the other aftward member. There is a variable-length member connected to the bootstrap-end of each of the two aftward members, with each of the variable-length members having a pivotable connection to the pylon.


    Access

    Download


    Export, share and cite



    Title :

    Engine installation system


    Contributors:

    Publication date :

    2017-08-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES



    ENGINE INSTALLATION SYSTEM

    MERCIER CLAUDE | European Patent Office | 2015

    Free access

    Engine installation

    Harrison, H.C. | Engineering Index Backfile | 1956


    Engine installation

    STRETTON RICHARD GEOFFREY | European Patent Office | 2016

    Free access

    Aircraft-Engine Installation

    NUTT, ARTHUR | SAE Technical Papers | 1930


    Aero-Engine Installation

    Pettitt-Herriot , J. A.RAe.S. | Emerald Group Publishing | 1934